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72 Cards in this Set
- Front
- Back
Branch of mechanics that studies the internal effects of stress and strain in a solid body that is subjected to an external loading. |
Mechanics of Materials |
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Deals with the relations between externally applied loads and their internal effects on the body |
Strength of materials |
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Defined as the strength of a material per unit area or unit strength. |
Stress |
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Former unit of stress |
psi (now in N/mm^2 or MPa) |
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Either the tensile or compressive stress |
Normal Stress or Axial Stress |
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__ will tend to shorten the member. |
Compression |
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__ will tend to lengthen the member |
Tension |
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Forces parallel to the area resisting the force cause __ |
Shearing Stress or Tangential Stress |
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Other types of shearing stress |
Punching shear Single shear Double shear |
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Contact pressure between the separate bodies. It is the internal stress caused by compressive forces |
Bearing stress |
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Also known as unit deformation. It is the ratio of the change in length caused by the applied force to the original length. Describes the geometry of deformation, independent of what actually causes the deformation |
Simple Strain |
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Characterizes dimensional changes |
Normal Strain |
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Describes distortion (changes in angles) |
Shear Strain |
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The testing machine that elongates the specimen at a slow, constant rate until the specimen ruptures. |
Tensile Test |
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Stress-Strain Diagram |
0 -- Proportional Limit Elastic Limit Yield Point -- Ultimate Strength -> Actual Rupture Strength Rupture Strength |
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Metallic engineering materials are classified as either __ or __ materials |
ductile - brittle |
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One having relatively large tensile strengths up to the point of rupture like structural steel and aluminum |
Ductile |
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Has a relatively small strain up to the point of rupture like cast iron and concrete |
Brittle |
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Arbitrary strain of __ is frequently taken as the dividing line between brittle and ductile classes |
0.05 mm/mm |
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Stress strain diagram is a straight line from the origin 0 to a point called the __. Beyond this point, stress is no longer proportional to strain. |
Proportional Limit |
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The stress-strain diagram is a manifestation of __ |
Hooke's Law |
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The stress-strain proportionality is assumed to exist up to a stress at which the strain __ at a rate of __ greater than shown by the initial tangent to the stress-strain diagram |
increases - 50% |
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This linear relation between elongation and the axial force causing was first noticed by __ in __ and is called __ that within the proportional limit, the stress is directly proportional to strain. |
Sir Robert Hooke - 1678 - Hooke's Law |
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Constant of proportionality E is called the __, a measure of the stiffness of a material. |
Modulus of Elasticity or Young's Modulus |
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The value of E is equal to __ |
Slope of the straight line. |
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The ratio of the steady force acting on an elastic body to the resulting displacement. |
Stiffness (k) |
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__ is the stress beyond which the material is no longer elastic. It is the value of stress on the stress-strain curve at which the material has deformed plastically |
Elastic Limit |
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The elastic limit is __ than the proportional limit |
slightly larger |
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The permanent deformation that remains after the removal of the load is called ___ |
Permanent set |
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A material is said to be __ if , after being loaded, the material returns to its original size and shape when the load is removed |
Elastic |
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The region in the stress-strain diagram from 0 to P. |
Elastic Range |
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The region from P to R. |
Plastic Range. |
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The point where the stress-strain diagram becomes almost horizontal is __ and its corresponding stress is __ |
Yield Point - Yield Stress or Yield Strength |
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The highest stress on the stress-strain diagram |
Ultimate strength |
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The maximum ordinate in the stress-strain diagram. |
Actual rupture strength or Tensile strength or Ultimate strength |
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The stress at which failure occurs |
Rupture strength or rupture stress |
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The strength of the material at rupture. |
Breaking strength |
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The Big Question: The nominal rupture strength (for structural strength) is considerably lower than the actual rupture strength. Why? |
Because the nominal rupture strength is computed by dividing the load at rupture by the original cross-sectional area. The actual rupture strength is calculated using the reduced area of the cross section where the fracture occurred. |
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The work done on a unit volume of material as the force is gradually increased from 0 to P |
Modulus of Resilience |
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The __ of a material is its ability to absorb energy without creating a permanent distortion |
Resilience |
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The work done on a unit volume of material as the force is gradually increased from 0 to R |
Modulus of Toughness |
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The __ of a material is its ability to absorb energy without causing it to break |
Toughness |
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Term describing the structural capacity of a system beyond expected or actual loads |
Factor of Safety |
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The maximum axial stress used in design |
Working Stress or Allowable Stress |
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Working stress should be limited to values __ so that the stresses remain in the __. |
not exceeding the proportional limit - elastic range |
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Because the proportional limit is difficult to determine accurately, it is customary to base the working stress on either the yield stress or the ultimate stress divided by a suitable number called __ |
Factor of Safety |
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The Big Question (2): Why is the yield stress easier to determine accurately than the proportional limit? |
For wider range of strain, yield stress does not vary significantly |
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__ causes shearing deformation |
Shearing forces |
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The change in angle at the corner of an original rectangular element is called __ |
Shear strain |
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The ratio of the shear stress and the shear strain is called __. |
Modulus of Elasticity or Modulus of Rigidity |
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__ showed that the ratio of the transverse strain to the axial strain is constant for stresses within the proportional limit. This constant is called __. |
Simeon D. Poisson (1811) - Poisson's ratio |
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Common values of Poisson's ratio are: __ for steel __ for other metals __ for concrete __ max |
Steel: 0.25 - 0.30 Others: 0.33 Concrete: 0.20 Max: 0.5 |
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The __ is uniform throughout the cross section and is the same in any direction in the plane of the cross section |
Transverse strain |
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__ is the shear modulus of elasticity (simple shear modulus), or the modulus of rigidity. (Pa or psi) |
G |
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Modulus of Elasticity (Young's Modulus) Formula |
E = Stress/Strain |
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Modulus of Rigidity (Shear Modulus) Formula |
G = Shearing Stress/Shearing Strain |
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Bulk Modulus Formula |
E = Volume Stress/Volume Strain |
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Measure of a resistance of a material to change in volume without change in shape or form |
Bulk modulus of elasticity (K) |
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If the equilibrium equations are sufficient to calculate all the forces (including support reactions) that act on a body, these forces are said to be __. |
Statically determinate |
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The number of unknown forces is __ to the number of independent equilibrium equations. |
always equal to |
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If the number of unknown forces exceeds the number of independent equilibrium equations, the problem is said to be __ |
Statically indeterminate |
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Mathematical expressions of geometric restrictions imposed on the deformation of statically indeterminate problems |
Compatibility Equations |
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Internal stress created |
Thermal stress |
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Pressurized container often cylindrical or spherical. |
Pressure vessel |
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Resist bursting forces developed across longitudinal and transverse sections. |
Tensile forces |
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The stress in the longitudinal section that resist the bursting force |
Tangential stress |
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Tangential stress is also called |
Circumferential stress Hoop stress Girth stress |
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Acts parallel to the longitudinal axis of the cylinder |
Longitudinal stress |
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Twisting of an object due to applied torque |
Torsion |
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Tendency of a force to rotate on an object about an axis (fulcrum or pivot); measure of resistance to twisting |
Torque |
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Modulus of rigidity; ratio of shear stress to shear strain; concerned with the deformation of a solid when it experiences a force parallel to one of its surfaces |
Shear Modulus |
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Quantity used to predict an object's ability to resist torsion |
Polar Moment or Inertia (J) |